Cooled heat shield for gas turbine combustor

• US 6,276,142 B1
• Filed: 02/18/2000
• Issued: 08/21/2001
• Est. Priority Date: 08/18/1997
• Status: Expired due to Term

• Current Assignee: Siemens AG
• Original Assignee: Siemens AG
• Inventors: Pütz, Heinrich
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US09/507,355
• Time in Patent Office: 550 Days
• Field of Search: 607/22, 607/52, 415/115, 415/116, 415/175
• US Class Current: 60/752
• CPC Class Codes: F05B 2260/201 by impingement of a fluid
• CPC Class Codes: F05B 2260/205 Cooling fluid recirculation, i.e. after having cooled one or more components the cooling fluid is recovered and used elsewhere for other purposes
• CPC Class Codes: F05B 2260/2241 using fins or ribs
• CPC Class Codes: F23M 5/02 characterised by the shape of the bricks or blocks used
• CPC Class Codes: F23R 2900/00012 Details of sealing devices
• CPC Class Codes: F23R 2900/03044 Impingement cooled combustion chamber walls or subassemblies
• CPC Class Codes: F23R 3/002 Wall structures F23R3/02 and F23R3/007 take precedence

Abstract

A heat-shield component with cooling-fluid return includes an outer hollow body and an insert that can both be mounted on a supporting structure. The outer hollow body encloses the insert with a gap. The outer hollow body has a first bottom side which can be exposed to a hot gas. The insert has a second bottom side with a plurality of holes through which the cooling fluid flows into the gap for impact-cooling the first bottom side. A heat-shield configuration for a hot-gas conducting component as well as a heat-shield assembly are also provided.

Claims

1. A gas turbine, comprising:

a combustion chamber with an inner wall acting as a supporting structure; and

a heat-shield configuration including a plurality of heat-shield components disposed next to one another for attachment to said supporting structure, each of said heat-shield components having;

an outer hollow body to be attached to the supporting structure, said outer hollow body having side walls and a first base side to be exposed to a hot gas;

an insert to be attached to the supporting structure, said insert enclosed by said outer hollow body and defining an intermediate space between said outer hollow body and said insert, said insert having side walls and a second base side with a plurality of openings for passage of cooling fluid into said intermediate space; and

a hot gas directing component wall to be exposed to a hot gas, said wall formed by said first and second base sides of said heat-shield component.

2. A gas turbine, comprising:

a combustion chamber having an inner wall acting as a supporting structure;

a heat-shield configuration including a plurality of heat-shield components disposed next to one another for attachment to said supporting structure, each of said heat-shield components having an outer hollow body to be attached to the supporting structure, said outer hollow body having side walls and a first base side to be exposed to a hot gas;

an insert to be attached to the supporting structure, said insert enclosed by said outer hollow body and defining an intermediate space between said outer hollow body and said insert, said insert having side walls and a second base side with a plurality of openings for passage of cooling fluid into said intermediate space; and

a hot gas directing component wall to be exposed to a hot gas, said wall formed by said first and second base sides of said heat-shield component;

said supporting structure having an inlet passage for cooling fluid in a region inside said side wall of said insert, and an outlet passage from said intermediate space for cooling fluid.

3. The heat-shield assembly according to claim 2, including a hot-gas space, a feed passage disposed outside said hot-gas space and connected to said inlet passage, and a discharge passage disposed outside said hot-gas space and connected to said outlet passage.

4. The heat-shield assembly according to claim 3, including a compressor feeding the cooling fluid through said feed passage to said heat-shield component.

5. The heat-shield assembly according to claim 4, including a burner receiving the cooling fluid from said discharge passage.